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Unmanned aerial vehicle, control system and method thereof, and unmanned aerial vehicle landing control method

a technology for unmanned aerial vehicles and landing control, which is applied in the direction of aircraft convertible vehicles, instruments, floats, etc., can solve the problems of limited pleasure from using existing unmanned aerial vehicles, unable to navigate on water, and unable to achieve amphibian functions

Active Publication Date: 2020-06-02
SZ DJI TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

This patent describes a supporting mechanism for an unmanned aerial vehicle that can adjust its distance from the body of the vehicle. The vehicle also has a rotor assembly that can be controlled to provide power for both aerial flight and navigation on water surfaces. The technical effects of this invention include improved stability and control of the unmanned aerial vehicle, as well as increased efficiency in its operation.

Problems solved by technology

However, the existing unmanned aerial vehicles can only be used as flight toys.
They can neither navigate on water, nor achieve an amphibian function either.
Therefore, the pleasure from using the existing unmanned aerial vehicles is limited.

Method used

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  • Unmanned aerial vehicle, control system and method thereof, and unmanned aerial vehicle landing control method
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  • Unmanned aerial vehicle, control system and method thereof, and unmanned aerial vehicle landing control method

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Embodiment Construction

[0255]The technical solution in embodiments of the present disclosure is described in detail below with reference to the accompanying drawings in the embodiments of the present disclosure. It is apparent that the embodiments described are merely some embodiments of the present disclosure instead of all the embodiments. Based on the described embodiments in the present disclosure, all other embodiments obtained by persons of ordinary skill in the art without creative efforts all belong to the scope of the present disclosure.

[0256]It should be noted that, when one component is referred to as “fixed to” another component, it may be directly on another component or it is also possible that there is a third component between them. When one component is considered to “connect” another component, it may be directly connected to the other component or it is possible that there is a third component between them. When one component is considered to be “disposed on” another component, it may b...

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Abstract

An unmanned aerial vehicle includes a fuselage, a power device connected to the fuselage, and a control device disposed at the fuselage and electrically connected with the power device. The control device is configured to control the power device to switch an operating mode of the power device to cause the unmanned aerial vehicle to fly in air or navigate on a water surface.

Description

CROSS-REFERENCE TO RELATED APPLICATION[0001]This application is a continuation application of International Application No. PCT / CN2015 / 083171, filed on Jul. 2, 2015, the entire contents of which are incorporated herein by reference.FIELD OF THE DISCLOSURE[0002]The present disclosure relates to an unmanned aerial vehicle, an unmanned aerial vehicle control system, an unmanned aerial vehicle control method, and an unmanned aerial vehicle landing control method.BACKGROUND[0003]A pilotless aircraft is called “unmanned aerial vehicle”, and is an unmanned aircraft manipulated by using a radio remote control apparatus and a self-contained program control device. Amphibian unmanned aerial vehicles are usually mainly used in aerial flight, and can perform a short navigation in the water when executing a task over water areas such as a sea surface. However, the existing unmanned aerial vehicles can only be used as flight toys. They can neither navigate on water, nor achieve an amphibian funct...

Claims

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Application Information

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Patent Type & Authority Patents(United States)
IPC IPC(8): B64C39/02B64C25/56G05D1/06G05D1/10
CPCG05D1/0676B64C39/024B64C25/56B64C2201/18B64C2201/024B64C25/66B64C35/00B60F5/02B64C25/58B64C25/60B64C25/62B64C35/005B64D43/00B64D47/02B64C2025/325B64U70/90B64U10/13B64U2101/30B64U30/20B64C35/008
Inventor WANG, MINGYU
Owner SZ DJI TECH CO LTD
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